N960FE1988 Cessna 208B
Safety record in brief:No NTSB accidents or incidents since 198211 ADs may apply5 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Federal Express Corporation
- Owner type
- Corporation
- City, state
- Memphis, TN
- Certificate issued
- Mar 28, 1988
- Expires
- Feb 28, 2030
- Airworthiness
- Standard · Normal
- Airworthiness date
- Mar 1, 1988
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Cessna
- Model
- 208B
- Year
- 1988
- Serial number
- 208B0075
- Aircraft type
- Fixed wing single engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 12
- Engines
- 1
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- AD5CA8
Engine
- Make and model
- P&W Pt6a Ser
- Type
- Turbo-prop
- Power
- 750 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 1988 – nowFederal Express CorporationMemphis, TN · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (11)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2021-04-10 | Textron Aviation, Inc. Airplanes | Apr 12, 2021 | Airframe (208B)Certain serial numbers: 208 20800564–20800594; 208 20800603–20800605; 208B 208B5141–208B5285; 208B 208B5287–208B5305; 208B 208B5307–208B5312; 208B 208B5314; … |
| 2009-15-05 | Cessna Aircraft Company Models 208 and 208B Airplanes | Jul 27, 2009 | Airframe (208B)Certain serial numbers: 208 20800500–20800504; 208B 208B1216; 208B 208B2001; 208B 208B2003–208B2023; 208B 208B2025–208B2029; 208B 208B2031–208B2037; … |
| 2009-05-12 | Cessna Aircraft Company Models 208 and 208B Airplanes | Apr 15, 2009 | Airframe (208B)Certain serial numbers: 208 20800001–20800415; 208 20800417–20800419; 208B 208B0001–208B1081; 208B 208B1083–208B1215; 208B 208B1217–208B1257; 208B 208B1259–208B1305; … |
| 2008-13-06 | Cessna Aircraft Company Models 208 and 208B Airplanes | Jul 30, 2008 | Airframe (208B)Certain serial numbers: 208 20800001–20800415; 208B 208B0001–208B1299 |
| 2008-10-02 | Cessna Aircraft Company 172, 175, 180, 182, 185, 206, 207, 208, 210, and 303 Series… | May 12, 2008 | Airframe (208B)Certain serial numbers: 172S 172S10672–172S10674; 172S 172S10676; 172S 172S10678–172S10680; 172S 172S10682; 172S 172S10683; 172S 172S10685; …. Only with: Applies only to airplanes that have a P/N 2013142-18 alternate static air source selector valve installed after November 19, 2007. |
Show all 11 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2007-10-15 | Cessna Aircraft Company Models 208 and 208B Airplanes | Jun 21, 2007 | Airframe (208B) |
| 2006-01-11 R1 | The Cessna Aircraft Company Models 208 and 208B Airplanes | Feb 22, 2006 | Airframe (208B) |
| 2004-08-17 | Cessna Aircraft Company Models 208 and 208B Airplanes | May 17, 2004 | Airframe (208B)Certain serial numbers: 208 20800370; 208 20800371; 208B 208B1034–208B1043; 208B 208B1045; 208B 208B1046; 208B 208B1048 |
| 2003-21-04 | Cessna Aircraft Company Models 208 and 208B Airplanes | Oct 21, 2003 | Airframe (208B)Certain serial numbers: 208 20800001–20800369; 208B 208B0001–208B1014; 208B 208B1017; 208B 208B1018; 208B 208B1020–208B1024; 208B 208B1026; … |
| 2002-22-17 | Cessna Aircraft Company Models 208 and 208B Airplanes | Dec 31, 2002 | Airframe (208B) |
| 97-25-04 | Cessna Aircraft Company Models 208, 208A, 208B, 425, and 441 Airplanes | Jan 21, 1998 | Airframe (208B) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (5)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Power plant · cowling · openSep 18, 2021
FLIGHT 8657, ENROUTE SEA-CLM AIR TURNBACK/DISCREPANCY: RIGHT COWLING OPENED IN FLIGHT RIGHT AFTER TAKEOFF. AIRCRAFT WAS RETURNED TO SEA. NO EMERGENCY DECLARED. LANDED WITHOUT FURTHER INCIDENT. CORRECTIVE ACTION: MAINTENANCE FOUND R/H UPPER ENGINE LATCH UNLATCHED. PERFORMED INSPECTIONS OF ENGINE…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · seat track · corrodedNov 2, 2011
INSP AT PDX - LEVEL 2 CORROSION: DURING INSPECTION, FOUND 5 CARGO AREA SEAT TRACKS CORRODED BEYOND SERVICEABLE LIMITS. DAMAGE IS MOSTLY FOUND BETWEEN FUSELAGE STATION 282 AND 332, HOWEVER, SOME DAMAGE DOES EXIST IN THE AREAS BETWEEN FUSELAGE STATION 166-332. REMOVED AND REPLACED CARGO SEAT TRACK…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Propellers · blade · strippedMay 12, 2008
STRIPPED OUT THREADS FOUND DURING MINI CHECK IN GEG: WHILE CHECKING FOR PROPER TORQUE ON THE PROPELLER BLADE ACTUATOR PIN (P/N B5072-1) ATTACHING SCREWS (P/N A-1635-159) ONE SCREW WAS UNABLE TO ACHIEVE PROPER TORQUE DUE TO STRIPPED OUT THREADS IN THE BLADE BUTT. REMOVED SCREW AND FOUND AN UNUSUAL…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 5 reportsShow fewer reports
- Electrical power · control unit · inoperativeDec 4, 2007
RETURNED TO BLOCKS: FLIGHT NR 8800, ON TAXI TO RUNWAY IN GEG STANDBY ELECTRIC GENERATOR FAULT LIGHT ILLUMINATED. ATTEMPTED RESET WAS UNABLE TO CLEAR THE FAULT, PILOT ELECTED TO RETURN TO RAMP. MAINTENANCE REMOVED AND REPLACED THE ALTERNATOR CONTROL UNIT. (K)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · retract mech · out of adjustAug 16, 1996
AFTER DEPARTURE FROM GEG, THE PILOT EXPERIENCED A NUMBER OF ELECTRICAL PROBLEMS. THE TRIM WARNING LIGHT AND HORN CAME ON. THE TRIM TEST BUTTON, ELECTRICAL TRIM CIRCUIT BREAKER, AND AUTOPILOT CIRCUIT BREAKER HAD NO EFFECT. THE FLAP MOTOR CIRCUIT BREAKER TRIPPED AND ODOR OF SMOKE. NO VISUAL EVIDENCE…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026